CN107591054A - Flight simulator emulation canopy frame and rearview mirror external member and flight simulator - Google Patents
Flight simulator emulation canopy frame and rearview mirror external member and flight simulator Download PDFInfo
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- CN107591054A CN107591054A CN201710948752.4A CN201710948752A CN107591054A CN 107591054 A CN107591054 A CN 107591054A CN 201710948752 A CN201710948752 A CN 201710948752A CN 107591054 A CN107591054 A CN 107591054A
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- rearview mirror
- display screen
- canopy frame
- flight simulator
- cockpit
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
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Abstract
The invention discloses a kind of flight simulator emulation canopy frame and rearview mirror external member and flight simulator, the flight simulator includes canopy frame and multiple rearview mirror assemblies with emulation canopy frame and rearview mirror external member；Canopy frame is used for the cockpit installed in flight simulator, so as to substitute cockpit windscreen frame as the orientation reference mark thing in cockpit visual field；Rearview mirror assemblies include display screen, connecting bracket and location aware module, and wherein display screen is fixed on the leading edge of canopy frame by connecting bracket, and location aware module is connected with display screen；Display screen and location aware module electrically connect with a main control computer.The alternative cockpit windscreen frame of canopy frame in the present invention is as the orientation reference mark thing in cockpit visual field, cockpit visual field can more accurately be reduced, and the display content of display screen changes with the change of its position in main control computer control rearview mirror assemblies, and pilot can be allowed to experience backsight scene more true to nature.
Description
Technical field
The present invention relates to flight simulator technical field, more particularly to a kind of flight simulator with emulation canopy frame and
Rearview mirror external member and flight simulator.
Background technology
Cockpit is the important component of piloted vehicle, and all kinds of flight simulators are in kind or HWIL simulation
Direct object.At present military flight simulator develop field, be all using cockpit windscreen frame as cockpit visual field in side
Position reference mark thing, but canopy is in buckling state actually in flight course, therefore really pilot view is played
Influence is canopy frame, and is not cockpit windscreen frame.Cockpit windscreen frame is compared with canopy frame no matter
It is in area coverage, or larger difference is present in the angle of sideline.Therefore made in flight simulator with cockpit windscreen frame
It is wrong for the orientation reference mark thing in cockpit visual field, and the reference mark of mistake certainly will cause the relation of mistake to sentence
It is disconnected, not only emphasize formation flight and approach etc. that observation produces many passive shadows with the synthetic flight training topic judged
Ring, be more artificially exaggerated training " negative transfer " effect.
In addition, important component of the rearview mirror as aircraft cabin, is that pilot visually grasps aircraft rear particularly just
The Main Means of rear situation.It not only causes pilot while tracking objects ahead closely, still to possess and keep constantly
The ability that rear is visually guarded against, moreover it is possible in the case where the motor-driven middle pilot of big overload is difficult to significantly rotate head, for its creation
Convenient and necessary backward observation condition.And kept in stream takeoff or landing, formation air refuelling, aerial flight pattern,
Especially serve as formation leader and take visual type commander to form into columns etc. and also play indispensable effect in flight operation process.
Therefore, canopy frame and rearview mirror are key element indispensable in cockpit simulated environment structure.But exist at present
Flight simulator develops field and does not occur the related design of Simulation about canopy frame also, and because rearview mirror is generally all set
The leading edge locus of canopy frame is placed in, therefore develops field in current flight simulator and does not also occur imitating about rearview mirror
True design.
The content of the invention
In view of the above-mentioned problems, the application provides a kind of flight simulator emulation canopy frame and rearview mirror external member, should
Flight simulator, which emulates canopy frame and rearview mirror external member, to be included：Canopy frame and multiple rearview mirror assemblies；
The canopy frame is used for the cockpit installed in flight simulator, so as to substitute cockpit windscreen frame as seat
Orientation reference mark thing in the visual field of cabin；
The rearview mirror assemblies include display screen, connecting bracket and location aware module, wherein the display screen passes through institute
The leading edge that connecting bracket is fixed on the canopy frame is stated, the location aware module is connected with the display screen, institute's rheme
Put the positional information that sensing module is used to detect the display screen；
The display screen and the location aware module electrically connect with a main control computer, and the main control computer is used for
Receive the positional information for the display screen that the location aware module is sent, and according to the positional information to the display screen
Send display information.
Alternatively, the quantity of the rearview mirror assemblies is three, and is located at the front and a left side of the cockpit visual field respectively
Right both sides.
Alternatively, the display screen is liquid crystal display.
Alternatively, the connecting bracket is twin shaft adjustable support.
Alternatively, the location aware module is double-shaft tilt angle sensor.
Alternatively, the display screen and the location aware module respectively by way of data/address bus with the master control meter
Calculate mechatronics.
In view of the above-mentioned problems, the application also provides a kind of flight simulator, the flight simulator includes above-mentioned flight mould
Intend device emulation canopy frame and rearview mirror external member.
The present invention emulates canopy frame and rearview mirror external member by designing a flight simulator, with canopy frame
Cockpit windscreen frame is substituted as the orientation reference mark thing in cockpit visual field, so that cockpit visual field more conforms to actual fly
Cockpit visual field in the case of row, cockpit visual field can be more accurately reduced, cockpit windscreen side is used in the prior art so as to avoid
The problem of frame is artificially exaggerated training " negative transfer " effect caused by as the orientation reference mark thing in cockpit visual field.And
The present invention controls the display content of display screen in rearview mirror assemblies to change with the change of its position by main control computer, can be with
Pilot is allowed to experience backsight scene more true to nature, so as to improve the simulation performance of flight simulator.
Brief description of the drawings
Fig. 1 is that the flight simulator of the embodiment of the present invention emulates canopy frame and the perspective view of rearview mirror external member；
Fig. 2 is the structural representation of the rearview mirror assemblies in the embodiment of the present invention.
Description of reference numerals：
1：Canopy frame back edge, 2：Windscreen frame back edge, 3：Rearview mirror assemblies,
4：Instrument board interface, 5：Canopy frame, 6：Display screen, 7：Location aware module,
8：Connecting bracket, 9：Main control computer.
Embodiment
To make the purpose, technical scheme and advantage of the embodiment of the present invention clearer, below in conjunction with the embodiment of the present invention
In accompanying drawing, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is
The part of the embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained on the premise of creative work is not made, belongs to the scope of protection of the invention.
Referring to Fig. 1, during practical flight, because canopy is in buckling state all the time, in cockpit visual field
In should include instrument board interface 4, canopy frame 5, rearview mirror assemblies 3 and cockpit windscreen frame, now to pilot view
Really play influence should be canopy frame 5, and not cockpit windscreen frame.As can be seen from Figure 1 in cockpit
The back edge 2 of cockpit windscreen frame is compared with the back edge 1 of canopy frame 5 in visual field, either in area coverage, or
Larger difference be present in the angle of sideline.
Therefore it is in the prior art wrong using cockpit windscreen frame as the orientation reference standard thing in cockpit visual field.And
The reference mark thing of mistake certainly will cause the relation of mistake to judge that this can be not only emphasized formation flight and approach etc.
Observation produces many negative influences with the synthetic flight training topic judged, can more produce artificial amplification training " negative transfer " effect
The problem of.
So to solve the above problems, the present embodiment provides a kind of flight simulator emulation canopy frame and rearview mirror
External member, the orientation reference mark in cockpit visual field is used as so as to substitute cockpit windscreen frame by the use of canopy frame 5 therein
Thing.The flight simulator, which emulates canopy frame and rearview mirror external member, to be included：Canopy frame 5 and multiple rearview mirror assemblies 3.
Wherein canopy frame 5 is used for the cockpit installed in flight simulator, so as to substitute cockpit windscreen frame conduct
Orientation reference mark thing in cockpit visual field, and rearview mirror assemblies 3 are then arranged on the leading edge locus of canopy frame 5, it is used for
The backsight environment during practical flight is simulated, the rearview mirror assemblies 3 determine configuration quantity according to the actual state of simulation object
And position, usually two to three, it is symmetrically arranged by reference of cockpit visual field median vertical line, such as when backsight microscope group
When the quantity of part 3 is three, it is located at the front and the left and right sides of cockpit visual field respectively, it is of course possible to understanding, this reality
Particular number and installation site that example does not limit rearview mirror assemblies 3 are applied, it needs to set its tool according to aircraft to be emulated
Body quantity and installation site.
Specifically, referring to Fig. 2, rearview mirror assemblies 3 include display screen 6, connecting bracket 8 and position sense in the present embodiment
Know module 7, wherein display screen 6 is used to show video information, so as to which optionally, it passes through company after simulating during practical flight
The leading edge that support 8 is fixed on canopy frame 5 is connect, location aware module 7 is connected with display screen 6, and it is used for the position to display screen 6
Confidence breath is detected, and determines the shift in position situation of display screen 6.
And in order to realize that the display information of display screen 6 can change with the change of its position, show in the present embodiment
Display screen 6 and location aware module 7 are electrically connected with a main control computer 9 by way of data/address bus, and main control computer 9 is used for
The positional information for the display screen 6 that receiving position sensing module 7 is sent, and according to the positional information of display screen 6 to corresponding display
Screen 6 sends display informations, so as to simulate after the pilot during live flying optionally.
Display screen 6 in wherein above-mentioned rearview mirror assemblies 3 is ultra-thin, the ultra-wide for meeting structure installation and profile simulation needs
The LCDs of type.Of course, it should be understood that the present embodiment does not limit the particular type of display screen 6.And connecting bracket 8
Twin shaft adjustable support is then selected, namely in cockpit visual field, by connecting bracket 8, the angle of display screen 6 is in X-direction and Y
It can be adjusted on direction of principal axis, have the connecting bracket that such function largely can be achieved in the market, as made in existing automobile
Driving mirror bracket is the support with such function be present, therefore for the concrete structure and Principles of Regulation of connecting bracket 8,
This is repeated no more.
What it is accordingly, due to the selection of connecting bracket 8 is twin shaft adjustable support, thus be accordingly used in detection display screen 6 position and becomes
The location aware module 7 of change can then select double-shaft tilt angle sensor, and double-shaft tilt angle sensor can be surveyed relative to two axles
Angle change, namely from Fig. 2, display screen 6 can be overturn in X-axis or Y direction, and sensing module 7 then can be to aobvious
Angle change of the display screen 6 in X-axis or Y direction is detected, and by the information transfer detected to main control computer 9, it is main
Control computer 9 is sent to different video informations according to the angle change of each display screen 6, during to live flying
After optionally emulated.
In addition, the present embodiment also provides a kind of flight simulator, the flight simulator includes above-mentioned flight simulator and used
Emulate canopy frame and rearview mirror external member.
The present embodiment emulates canopy frame and rearview mirror external member by designing a flight simulator, with canopy side
Frame substitutes cockpit windscreen frame as the orientation reference mark thing in cockpit visual field, so that cockpit visual field more conforms to reality
Cockpit visual field under flight progress, cockpit visual field can be more accurately reduced, cockpit windscreen is used in the prior art so as to avoid
The problem of frame is artificially exaggerated training " negative transfer " effect caused by as the orientation reference mark thing in cockpit visual field.And
And emulation canopy frame in the present embodiment and rearview mirror external member pass through main control computer and control display screen in rearview mirror assemblies
Display content change with the change of its position, pilot can be allowed to experience backsight scene more true to nature, so as to improve
The simulation performance of flight simulator.
It should be noted that herein, term " comprising ", "comprising" or its any other variant are intended to non-row
His property includes, so that process, method, article or terminal device including a series of elements not only will including those
Element, but also the other element including being not expressly set out, or it is this process, method, article or terminal also to include
The intrinsic key element of equipment.In the absence of more restrictions, the key element limited by sentence "including a ...", is not arranged
Except other identical element in the process including the key element, method, article or terminal device being also present.
The preferred embodiments of the present invention are these are only, are not intended to limit the invention, for those skilled in the art
For member, the present invention can have various modifications and variations.Any modification within the spirit and principles of the invention, being made,
Equivalent substitution, improvement etc., should be included in the scope of the protection.
Claims (7)
1. a kind of flight simulator emulation canopy frame and rearview mirror external member, it is characterised in that including：Canopy frame and
Multiple rearview mirror assemblies；
The canopy frame is used for the cockpit installed in flight simulator, is regarded so as to substitute cockpit windscreen frame as cockpit
Orientation reference mark thing in；
The rearview mirror assemblies include display screen, connecting bracket and location aware module, wherein the display screen passes through the company
The leading edge that support is fixed on the canopy frame is connect, the location aware module is connected with the display screen, the position sense
Know that module is used for the positional information for detecting the display screen；
The display screen and the location aware module electrically connect with a main control computer, and the main control computer is used to receive
The positional information for the display screen that the location aware module is sent, and sent according to the positional information to the display screen
Display information.
2. flight simulator as claimed in claim 1 emulation canopy frame and rearview mirror external member, it is characterised in that described
The quantity of rearview mirror assemblies is three, and is located at the front and the left and right sides of the cockpit visual field respectively.
3. flight simulator as claimed in claim 1 emulation canopy frame and rearview mirror external member, it is characterised in that described
Display screen is liquid crystal display.
4. flight simulator as claimed in claim 1 emulation canopy frame and rearview mirror external member, it is characterised in that described
Connecting bracket is twin shaft adjustable support.
5. flight simulator as claimed in claim 4 emulation canopy frame and rearview mirror external member, it is characterised in that described
Location aware module is double-shaft tilt angle sensor.
6. flight simulator as claimed in claim 1 emulation canopy frame and rearview mirror external member, it is characterised in that described
Display screen and the location aware module are electrically connected by way of data/address bus with the main control computer respectively.
7. a kind of flight simulator, it is characterised in that the flight simulator includes flying as described in claim any one of 1-6
Row simulator emulation canopy frame and rearview mirror external member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710948752.4A CN107591054B (en) | 2017-10-12 | 2017-10-12 | Simulation canopy frame and rearview mirror suite for flight simulator and flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710948752.4A CN107591054B (en) | 2017-10-12 | 2017-10-12 | Simulation canopy frame and rearview mirror suite for flight simulator and flight simulator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107591054A true CN107591054A (en) | 2018-01-16 |
| CN107591054B CN107591054B (en) | 2023-07-25 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710948752.4A Active CN107591054B (en) | 2017-10-12 | 2017-10-12 | Simulation canopy frame and rearview mirror suite for flight simulator and flight simulator |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108648558A (en) * | 2018-06-22 | 2018-10-12 | 中国人民解放军国防科技大学 | Manned and unmanned aerial vehicle collaborative drilling simulation cabin |
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| CN108648558B (en) * | 2018-06-22 | 2020-06-26 | 中国人民解放军国防科技大学 | Manned and unmanned aerial vehicle collaborative drilling simulation cabin |
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| Publication number | Publication date |
|---|---|
| CN107591054B (en) | 2023-07-25 |
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Effective date of registration: 20230915 Address after: Room 1607, 16th Floor, South Building, Qidi Cluster Innovation Building, No. 118 Rongtong Road, Binhai Street Office, Huangdao District, Qingdao City, Shandong Province, 266404 Patentee after: Hanke Zhixiang (Qingdao) Technology Development Co.,Ltd. Address before: No. 167, 2nd Floor, Main Building, No. 6 # -9 #, No. 59 Banjing Road, Haidian District, Beijing, 100089 Patentee before: Beijing Hanke Technology Group Co.,Ltd. |
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